View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 46906U 26145.59448808 +.00000000 +00000-0 +27068-3 0 00008
2 46906 36.8933 198.3818 0001511 339.0158 21.0529 15.26317351 07
| Epoch (UTC): | 25 May 2026 14:16:03 |
| Eccentricity: | 0.0001511 |
| inclination: | 36.8933° |
| perigee height: | 486 km |
| apogee height: | 488 km |
| right ascension of ascending node: | 198.3818° |
| argument of perigee: | 339.0158° |
| revolutions per day: | 15.26317351 |
| mean anomaly at epoch: | 21.0529° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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